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    Closure to “Discussion of ‘The Lomakin Effect in Annular Gas Seals Under Choked Flow Conditions’ ” (2007, ASME J. Eng. Gas Turbines Power, 129 , p. 1143)

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004::page 1144
    Author:
    Mihai Arghir
    DOI: 10.1115/1.2718219
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The authors are grateful for this experimental validation of the negative direct static stiffness of choked annular seals. For performing our own calculations, the mentioned conditions were supplemented by some additional assumptions that are somewhat usual for straight annular seals, namely, an imposed inlet pressure drop coefficient ζinlet and an exit recovery coefficient ζexit=1 (complete pressure recovery). The rotation speed was ω=0, and the flow regime was considered as being nonisothermal with adiabatic walls and Tinlet=20°C. Moody’s friction factor was used with the possibility of bridging transition between laminar and turbulent flow. The employed grid had 16 equally spaced cells in the axial direction and 32 in the circumferential one (Fig. 1).
    keyword(s): Flow (Dynamics) AND Gas turbines ,
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      Closure to “Discussion of ‘The Lomakin Effect in Annular Gas Seals Under Choked Flow Conditions’ ” (2007, ASME J. Eng. Gas Turbines Power, 129 , p. 1143)

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    contributor authorMihai Arghir
    date accessioned2017-05-09T00:23:33Z
    date available2017-05-09T00:23:33Z
    date copyrightOctober, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26973#1144_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135650
    description abstractThe authors are grateful for this experimental validation of the negative direct static stiffness of choked annular seals. For performing our own calculations, the mentioned conditions were supplemented by some additional assumptions that are somewhat usual for straight annular seals, namely, an imposed inlet pressure drop coefficient ζinlet and an exit recovery coefficient ζexit=1 (complete pressure recovery). The rotation speed was ω=0, and the flow regime was considered as being nonisothermal with adiabatic walls and Tinlet=20°C. Moody’s friction factor was used with the possibility of bridging transition between laminar and turbulent flow. The employed grid had 16 equally spaced cells in the axial direction and 32 in the circumferential one (Fig. 1).
    publisherThe American Society of Mechanical Engineers (ASME)
    titleClosure to “Discussion of ‘The Lomakin Effect in Annular Gas Seals Under Choked Flow Conditions’ ” (2007, ASME J. Eng. Gas Turbines Power, 129 , p. 1143)
    typeJournal Paper
    journal volume129
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2718219
    journal fristpage1144
    identifier eissn0742-4795
    keywordsFlow (Dynamics) AND Gas turbines
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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